|Publication number||US7775833 B1|
|Application number||US 12/163,507|
|Publication date||Aug 17, 2010|
|Filing date||Jun 27, 2008|
|Priority date||Jun 27, 2008|
|Publication number||12163507, 163507, US 7775833 B1, US 7775833B1, US-B1-7775833, US7775833 B1, US7775833B1|
|Inventors||Kevin D. Le, Ricardo Ramirez, Kisoo Jung|
|Original Assignee||Williams Pyro, Inc.|
|Export Citation||BiBTeX, EndNote, RefMan|
|Patent Citations (5), Referenced by (6), Classifications (4), Legal Events (5)|
|External Links: USPTO, USPTO Assignment, Espacenet|
This invention was made with government support under Contract No. HQ0006-06-C-7480 between the Missile Defense Agency section of the U.S. Department of Defense and Williams-Pyro, Inc. The government has certain rights in the invention.
The present invention relates generally to lightweight flexible cabling. More particularly, the present invention relates to multi-functional, high speed intelligent cables.
Transferring signals via cables or wires remains a preferred and a reliable mode for many applications, despite the advent of wireless means for transferring signals. Generally, cables are made of electrically conducting materials such as copper, aluminum, etc. and are shielded by an insulating material such as rubber or plastic for protection and safe handling. Cables that are used in high-end sophisticated systems such as satellite electronic harness systems may need to have, and may be required to have, capability to withstand extreme conditions such as high temperature and electromagnetic interference (EMI).
Conventional satellite electronic harness configurations utilize heavy and cumbersome cabling. These types of cables require heavy brackets to properly install, and consume a significant portion of the satellite's payload budget. Applications, other than satellites, can have similar volume and mass considerations. Marine equipment, unmanned spacecraft, and even commercial passenger aircraft can have a need for lightweight flexible cabling.
Flexible cabling can conform to the walls of a structure for mounting. Flexible cabling can easily bend into curvaceous paths. Less stress is induced on flexible lightweight cabling that bends as compared to conventional cabling, yielding increased life for a flexible cable that is mounted in a bent configuration. Flat cables can provide connection with low vertical clearance.
Conventional cabling may not afford self-diagnostic identification of a non-conducting line. Conventional cables may not facilitate system level integration and do not have test and diagnostic capability.
The components associated with conventional cabling, such as that for a satellite, compose a significant portion of the vehicle mass. Conventional cabling is labor intensive with respect to, for example, manufacturing. Further, conventional cabling systems are difficult to install in a vehicle and require bulky support brackets and terminations. In view of these characteristics, it is easy to see that a microscopically small flat and flexible cable could greatly reduce, for example, satellite weight. Other applications could also benefit from a reduction in the weight and volume of electronic system components, while maintaining or even improving system reliability. A flat flexible cable could be mounted within the walls of a structure.
System integration is not conventionally facilitated by the cables themselves. Bulky black boxes are conventionally used at interconnect and integration points. Cable installation and diagnostics and performance tests on installed cables or pre-installed cables can be labor intensive and time consuming.
The present invention provides a multi-functional high speed intelligent cable that may ultimately replace bulky black boxes and cables with a lightweight system that can be mounted on the structural wall of the vehicle.
One aspect of the present invention is a flexible high speed connection, which can readily conform to bends and curves resulting in low stress induced by a curved mounting configuration and ease of installation due to the flexibility of the cable, a multi-flex ribbon cable. A multi-functional cable assembly comprising a multi-flex cable in accordance with the present invention may have reduced cable fatigue from, in part, its flexibility and/or its low weight.
Another aspect of the present invention is the low vertical profile which provides low clearance and installation in space restricted environments.
Another aspect of the present invention is the resulting low mass for an increased functionality, positively contributing to the mass fraction payload ratio of, for example, a satellite vehicle.
Another aspect of the present invention is that it comprises built-in health indicators for ready assessment of, for example, connectivity.
Yet another aspect of the present invention is active electronics and embedded intelligent firmware.
Yet another aspect of the present invention is built-in test performance capability.
Still another aspect of the present invention is easy reconfiguration of the cable for system integration, or for other needs. Still further, built-in automatic multi-functional cable testing may also include automatic reconfiguration.
A cable in accordance with an exemplary embodiment of the present invention may require less touch labor and reduced time and labor for maintenance testing and scheduled, or otherwise desired, reconfigurations.
Another aspect of the present invention may be the ease of manufacturing. For example, slap-shielding is used for electromagnetic interference shielding of the entire cable as opposed to a conventional shielding of individual lines. The benefits of this aspect of the present invention are even greater as compared to micro-shielded cables.
Embodiments of the present invention may employ a unique built-in test capability. With integrated circuits and advanced software algorithms, a cable assembly in accordance with the present invention can check all the conductors in the flex cable for discontinuity or damage, and may reconfigure itself when activated by software and/or hardware. Further, in some embodiments, a satellite communication channel can be used to remotely activate a cable test and reconfiguration of a cable installed in a satellite from earth.
The detailed description is presented with reference to the accompanying figures. Like numbers across drawings may reference like features and components, but may vary across embodiments. For more complete understanding of the features and advantages of the present invention, reference is now made to the detailed description of the invention along with the accompanying figures, wherein:
The invention, as defined by the claims, may be better understood by reference to the following detailed description. The description is meant to be read with reference to the figures contained herein. This detailed description relates to examples of the claimed subject matter for illustrative purposes, and is in no way meant to limit the scope of the invention. The specific aspects and embodiments discussed herein are merely illustrative of ways to make and use the invention, and do not limit the scope of the invention.
An exemplary feature of a multi-functional multi-flex cable in accordance with an embodiment of the present invention is automatic built-in testing and reconfiguration with health indicators, which may significantly reduce touch labor and time for cable checkout during satellite integration. Health, or integrity status indicators may be, for example, light emitting diodes (LEDs). If degraded signal lines are found, the cable can reconfigure for desired performance. Further, in some embodiments, the cable test and reconfiguration can be remotely activated. For example, remote testing and reconfiguration can be between earth via the satellite communication channel to a satellite during an ongoing satellite mission.
More particularly, logic circuitries can enable automatic built-in test and reconfiguration of the multi-flex cables. If degraded signal lines are found during testing, the defective cable may be automatically re-configured. This can significantly reduce labor and time for cable checkout during sensitive operations, such as satellite integration. The cable's logic circuitries can be remotely activated from earth via satellite communication channel during a satellite mission. In yet another embodiment, testing results may be provided to a user for subsequent additional reconfiguration, initial configuration input, or for user-directed reconfiguration.
In one implementation, the cable assembly 100 also includes a logic circuitry 104 at both the ends of the cable 102. In another implementation, the logic circuitry 104 can be located at a remote end and can communicate with the cable 102 via a wired or wireless mechanism.
The logic circuitry 104 includes active electronics and embedded firmware for managing the cable 102. The logic circuitry 104 tests for and diagnoses faults that may occur in the cable 102. Further, the logic circuitry 104 may re-configure the cable 102 automatically when activated by a software or hardware to render the cable 102 free of faults and thus ensure smooth transmission of signals. In certain applications, such as space applications, the software or hardware can be remotely activated, such as from earth, via a satellite communication channel.
The logic circuitry 104 forms a part of a circuitry that includes one or more health indicators 106 and a test switch 108. The health indicators 106 may be visual means that give information about the health status of the cable 100. In one implementation, the health indicators 106 can be in the form of LEDs that indicate the health status or operating condition of the cable 102 by, for example, different colors. The health indicators 106 indicate, for example, whether the cable 102 is healthy, reparable, or irreparable. The test switch 108 is a switch that can be pushed for initiating a test procedure for the cable 102. While the multi-functional cable of
A cross-section of a segment 200 of the cable 102 is shown in
After the EMI shielding layer 214-1, there is a second insulation layer 212-2, similar to the insulation layer 212-1. Another EMI shielding layer 214-2, similar to the EMI shielding layer 214-1, is provided after the insulation layer 212-2. Next in the row is an inner insulation layer 216 that embeds several micro-conductors 208-1 to 208-N, collectively referred to as micro-conductors 208, which comprise signal lines 103.
In one implementation, the inner insulation layer 216 can be made of a thermosetting polyimide material such as Kapton polyimide film (Dupont Corporation, Wilmington, Del., USA). In one embodiment, the micro-conductors 208 can have a diameter of about 120 micrometers and can be made of materials with high electrical conductivity such as copper. The total thickness of the cable 102 can be around 350 micrometers, with the EMI shielding layers 214-1 and 214-2 having a thickness of approximately 50 microns each.
It is to be noted that a cable 102, in accordance with embodiments of the present invention, has low volume and mass, and is flat and flexible to conform easily to structural curvatures of the system in which the cable 102 is installed. A cable 102 can be made using simple fabrication techniques contributing to low cable costs. Moreover, EMI shielding and multiple micro-conductors may provide a higher speed of data transmission through the cable 102.
A CPLD may include a connector for an external power supply of 5 VDC. However, the CPLD also has the ability to obtain its operational power straight from data lines. In order to program a CPLD used in accordance with exemplary embodiments of the present invention, IEEE 1532 and the IEEE 1149.1 standards can be used in the respective logic circuitries 104. A 133 MHz oscillator can serve as a clock for the logic circuitries 104. In alternate embodiments, alternate clock sources may be incorporated. The voltage regulator used in the logic circuitries 104 can be an ultra low-dropout (LDO) regulator.
The logic circuitries 104-1 and 104-2 form part of a circuitry that includes their respective health indicators 106-1 and 106-2, and test switches 108-1 and 108-2. The circuitry also includes an interconnect switching circuitry 304, which is placed in the path of the cable 102 between the logic circuitries 104-1 and 104-2
The interconnect switching circuitry 304 allows self-testing and re-configuration in case of a fault or damage on any signal line 103 or micro-conductor of the cable 102. The interconnect switching circuitry 304 can switch a faulty line with a spare line and thus ensures smooth transmission of data through the cable 102. At the terminating end of the cable assembly, such as after the logic circuitry 104-2, the signal on the cable 102 is transmitted across a load with supply voltages 306-1 and 306.
In one implementation, for testing purpose, for example, the logic circuitries 104-1 and 104-2 in the cable assembly are configured as master and slave nodes. Either of the two logic circuitries 104 can serve as a master and the other end serves as a slave. The firmware for the testing can reside in either or both of the master and slave nodes.
With reference to the diagram 402, the master remains in an initial state, i.e. state 0 unless the test switch 108-1 is pushed, thereby providing a test signal in high logic state to the hardware or firmware in the master node. Once the test is started, the master enters state 1. In state 1, the master instructs the slave to perform tests as per specified conditions. As soon as the slave recognizes the testing condition from the master, the master enters state 2. Until the test is completed, the master remains in the state 2. Once the slave completes the test, the slave intimates the master of the completion of the tests. On receiving the intimation, the master returns to state 0. A reset signal 406 can reset the master at anytime and force the master to return to state 0.
With reference to the diagram 404, the slave remains in an initial state, i.e. state 0 unless a test request is received from the master. On receiving a test request from the master, the slave enters state 1. In state 1, the slave recognizes a test condition communicated by the master and when it has recognized the test condition, it leaves state 1 and enters state 2. In state 2, the slave recognizes a pattern for a continuity test for checking a faulty signal line.
Thereafter, the slave enters state 3 where it performs the continuity test for all the signal lines 103 on the cable 102. After completing the continuity test, the slave enters state 4. In state 4, the slave intimates the master about broken or faulty signals lines and with this, the slave completes the test and returns to state 0. A reset signal 408 can reset the slave at anytime and force the slave to return to state 0.
At block 502, the information stored on a printed circuit board (PCB) of the cable assembly is read. In one implementation, the logic circuitry 104 reads information such as state of the test switch 108 and configuration status to identify a master node and a slave node.
At block 504, the information read from the PCB is registered or passed onto the input bus of the PCB. In one implementation, the information read by the logic circuitry 104 is provided to the input bus connecting the logic circuitry 104 to the cable 102.
At block 506, state of a counter is compared to the total number of signal lines (N) in the multi-flex cable. In one implementation, a counter is initialized to unit value and is incremented after testing of a signal line 103 is completed.
At block 508, the value of the counter is compared with the total number of signal lines (N) 103 in the cable 102. If the value of the counter is found to be greater than N, then further testing is stopped at block 508. If value of the counter is less than N, then instructions at block 510 onwards are executed.
At block 510, a signal line corresponding to the value of the counter is tested and the output at the signal bus is checked. In one implementation, if the value at the output of the signal bus for a particular counter value is one, then the instructions at block 512 are executed; else the instructions at block 514 are executed.
At block 512, it is indicated that the signal line is perfect. In one implementation, one of health indicators 106, that may be in the form of a green LED, turn on if no fault is detected on any signal line 103 of the cable 102.
At block 514, it is checked whether the number of errors detected are more than the number of spare lines available in the multi-flex cable. In one implementation, the total number of errors that can be handled depends on the number of spare lines available in the cable 102. The logic circuitry 104 keeps a track of the number of errors on signal lines 103 encountered during the testing phase.
In case the number of errors is greater than the number of spare lines, then at block 516, the signal line may be declared faulty by, for example, turning on a red health indicator 106, as the cable cannot be completely re-configured in such a case for full continuity. If the number of errors is less than the number of spare lines available in the cable 102, then the instructions at block 518 are executed.
At block 518, it is indicated that at least one link in the multi-flex cable is broken or faulty. In one implementation, the health indicators 106 turn yellow indicating a fault in one or more signal lines 103 that can be rectified.
At block 520, a broken or faulty link, signal line, or micro-conductor, in the cable is reconfigured. In one implementation, a nearest spare line or link is determined for re-configuration of the faulty signal line in the cable 102. As soon as the spare link is found, an automatic connection is made by switching the signal path with using the switching circuitry 304.
Using a slap-shielding technique, a cable, in accordance with the present invention, with multiple conductors can be EMI shielded, resulting in a high-density interconnect that allows for high-speed data communications. A flat and flexible cable, in accordance with exemplary embodiments of the present invention, can smoothly conform to the satellite structure and transfer less mechanical stress, thus minimizing cable fatigue. Multi-functional multi-flex cables may significantly reduce system complexity and payload.
The multi-functional multi-flex high speed intelligent cable may have low production cost, can be reliable, and may be easy to fabricate and install. Implementing slap EMI shielding in multi-flex cable can eliminate complicated and expensive coating processes associated with fabricating conventional individually EMI-shielded cables, especially in micro-shielded cables. By using snap-in connectors, flat cables allow connectors to be installed without special skill or handling.
Built-in test capability contributes to the uniqueness of a cable in accordance with the present invention, among other cabling options. With integrated circuits and advanced software algorithms, a multi-functional cable, in accordance with exemplary embodiments of the present invention, can check all the conductors in the multi-flex cable for discontinuity or damage. Further, the cable can even reconfigure itself when activated by software or hardware, in accordance with embodiments of the present invention.
Although embodiments for a self-managing cable assembly have been described in language specific to structural features and/or methods, it is to be understood that the appended claims are not necessarily limited to the specific features or methods described. Rather, the specific features and methods are disclosed as exemplary implementations. While specific alternatives to steps of the invention have been described herein, additional alternatives not specifically disclosed but known in the art are intended to fall within the scope of the invention. Thus, it is understood that other applications of the present invention will be apparent to those skilled in the art upon reading the described embodiment and after consideration of the appended claims and drawings.
|Cited Patent||Filing date||Publication date||Applicant||Title|
|US4508399 *||Jan 3, 1984||Apr 2, 1985||Amp Incorporated||Polarized ribbon cable connector having circuit components therein|
|US4853626 *||Mar 8, 1988||Aug 1, 1989||Xilinx, Inc.||Emulator probe assembly for programmable logic devices|
|US5470238 *||Feb 9, 1994||Nov 28, 1995||Intercon Systems, Inc.||Shielded ribbon cable electrical connector assembly and method|
|US5571994 *||Jan 18, 1994||Nov 5, 1996||Norton; Peter||Weatherproof seal for wire entrance|
|US7477159 *||Sep 13, 2006||Jan 13, 2009||Hannspree Inc.||Detection device and method thereof|
|Citing Patent||Filing date||Publication date||Applicant||Title|
|US8172618 *||Nov 17, 2010||May 8, 2012||Ceramate Technical Co., Ltd.||Semiconductor-type electric connector|
|US9193313 *||Mar 22, 2013||Nov 24, 2015||Nuax, Inc.||Methods and apparatuses involving flexible cable/guidewire/interconnects|
|US20110061933 *||Mar 11, 2010||Mar 17, 2011||Apple Inc.||Flat cable for use with an electronic device|
|US20130221988 *||May 30, 2012||Aug 29, 2013||Apple Inc.||Devices and methods for testing flex cable shielding|
|US20150266436 *||Mar 22, 2013||Sep 24, 2015||Cardia Access, Inc.||Methods and apparatuses involving flexible cable/guidewire/interconnects|
|WO2014149155A1 *||Jan 10, 2014||Sep 25, 2014||Cardia Access, Inc.||Methods and apparatuses involving flexible cable/guidewire/interconnects|
|Jun 27, 2008||AS||Assignment|
Owner name: WILLIAMS-PYRO, INC., TEXAS
Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:LE, KEVIN D;RAMIREZ, RICARDO;JUNG, KISOO;SIGNING DATES FROM 20080626 TO 20080627;REEL/FRAME:021164/0315
|Nov 22, 2013||AS||Assignment|
Owner name: WILLIAMSRDM, INC., TEXAS
Free format text: CHANGE OF NAME;ASSIGNOR:WILLIAMS-PYRO, INC.;REEL/FRAME:031711/0167
Effective date: 20131015
|Mar 28, 2014||REMI||Maintenance fee reminder mailed|
|Aug 17, 2014||LAPS||Lapse for failure to pay maintenance fees|
|Oct 7, 2014||FP||Expired due to failure to pay maintenance fee|
Effective date: 20140817